• 한국컴퓨터정보학회논문지
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• 제15권4호
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• pp.99-106
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• 2010

본 논문에서는 MFC(Mass Flow Controller) 유닛으로부터 전송된 유체의 압력을 모니터하고 흐름 제어 기능을 수행하는 유체 유동 모니터링 시스템을 제안한다. 이 시스템은 MFC 유닛과 채널 디바이스, 모니터 및 관리 소프트웨어로 구성된다. MFC 유닛은 유체 압력 값을 측정하여 채널 디바이스로 전송하고, 채널 디바이스는 MFC 유닛과 모니터 및 관리 소프트웨어간의 입출력 인터페이스를 제공하는 기능을 한다. 모니터 및 관리 소프트웨어는 각 채널의 MFC 유닛에서 실시간으로 측정한 유체 압력 값을 모니터링하여 분석하고 제어한다. 이 소프트웨어는 20개의 채널과 0.1의 모니터링 주기로 구성하여 1초당 200개 즉, 1시간당 72만개의 데이터를 처리한다. 이때 입력 데이터 수의 증가에 따라 저장 공간도 비례하여 증가한다. 이러한 데이터 수의 증가와 저장 공간의 증가는 데이터 조회 성능을 저하시키기 때문에 데이터를 효율적으로 관리할 수 있는 변경값 감지 기법과 변경 범위 감지 기법으로 구현한다.

• 한국항공우주학회지
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• 제36권6호
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• pp.532-540
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• 2008

최근 구조변형을 고려한 항공기의 공력특성을 계산하는데 필요한 CFD와 CSD 기법이 연계된 FSI 시스템에 관한 관심이 증대하고 있다. 본 연구에서는 유체유발 구조 변형을 고려한 수렴된 구조형상에 대한 공력특성 예측을 위해 유체-구조 연계 시스템인 FSI(Fluid- Structure Interaction)를 구축하였다. 각 모듈의 연계, 특히 CSD와 CFD의 결합 및 변형된 형상에 대한 공력격자 재생성을 위해 VSI(Volume Spline Interpolation)와 격자 변형 코드를 개발하였으며, 공력과 구조의 해석 모듈로 상용 프로그램인 FLUENT와 NASTRAN을 사용하였다. 구축된 시스템을 DLR-F4 날개에 적용하여 정적 유체-구조 연구를 수행하였으며, 그 결과 마하수 0.75에서 변형된 형상에 대한 양력 및 항력 계수는 약 20.26%, 18.5% 감소하는 것으로 나타났다.

• 한국환경보건학회지
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• 제28권5호
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• pp.13-21
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• 2002

This study analyzed the characteristic of basic river structure, a flood level, the tree planting recommendation and syn thetic design, in order to establish a basic plan for preparing a natural practical area of environmental ecosystem at Bukchun and its surroundings. It was also investigated based on the opinion of citizens, geographical condition and the equipment/utilization examination of Bukchun which were included ecological circumstances, and thus provided a composite item for managing the natural river. This study also considered the development of the river in terms of culture, environment and ecology concept. The results were summarized as followed. Bukchun showed that the speed of a funning fluid is very fast on a period of flood. but very slow in a period of water shortage about 0.02 m/s. To prevent the speed change of a running fluid by a steep slope in a riverbed, there established Dongchun sluice gates under a bridge, including three sluice gates under a bridge, but there occurred extremely a riverbed erosion and corrosion section. The result of comparison between real flood degree and prediction flood data, there should perform a countermeasure the riverbed structure regulation of this area. Also, it was needed an exhaustive flood management in summer. According to the Bukchun and Hyungsangang riverbed investigation, there were needed preparation for natural/practical area and ecology Park development in the future. This study was investigated tree Planting/flower/blossom around the Bukchun and its surroundings. It was recommended willow, Italian poplar, bamboos and cherry blossoms in the Hyungsangang and Bukchun. There exist together historical space, environment space iud have enough possibility both natural learning space and civil rest space. And, it is possible to compose ecology natural learning and experimental area.

• 대한전자공학회:학술대회논문집
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• 대한전자공학회 2003년도 하계종합학술대회 논문집 V
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• pp.2713-2716
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• 2003

This paper presents a dynamic manipulability analysis method of the limb moving in viscous fluid. The key idea of the presented method is that the boundary of joint velocity can be converted to the velocity-dependant dynamic manipulability polytope through the coriolis, centrifugal and drag terms in dynamic equation. The velocity-dependant dynamic manipulability polytope is added to the inertial and restoring force manipulability polytope to get overall manipulability polytope of the limb moving in the fluid Each of the torque and velocity bounds arc considered in the infinite norm sense in joint space, and the drag force of a limb moving in fluid viscous is modeled as a quadratic form An analysis example with proposed analysis scheme is presented to validate the method.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2005년도 창립60주년 기념 추계 학술대회
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• pp.257-261
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• 2005

Over the past 30 years, numerical methods and simulation tools for fluid dynamic problems have advanced as a new discipline, namely, computational fluid dynamics (CFD). Although a wide spectrum of flow regimes are encountered in many areas of science and engineering, simulation of compressible flow has been the major driver for developing computational algorithms and tools. This Is probably due to a large demand for predicting the aerodynamic performance characteristics of flight vehicles, such as commercial, military, and space vehicles. As flow analysis is required to be more accurate and computationally efficient for both commercial and mission-oriented applications (such as those encountered in meteorology, aerospace vehicle development, general fluid engineering and biofluid analysis) CFD tools for engineering become increasingly important for predicting safety, performance and cost. This paper presents the author's perspective on the maturity of CFD, especially from an aerospace engineering point of view.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 1995년도 창립기념학술대회
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• pp.38-43
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• 1995

Effect of visualization as a tool for the education of fluid dynamics is mainly discussed. Visualized images are much more understandable compared to the explanation using equations and texts. Several examples are presented to clarify this statement. Then, the software system for teaching fluid dynamics using the results by the numerical simulation is discussed. Two important issues on what is needed in the system are given. First, such systems should be capable of animating images. Second, such systems should be interactively used by students. Changing parameters, coefficients, equations, etc. themselves and watching the difference are important for them to understand the nature of physics underlying the equations. The teaching system with visualization is no doubt a good tool for introducing fluid dynamics.

• 한국전산유체공학회지
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• 제3권2호
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• pp.1-8
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• 1998

We make use of cubic B-spline interpolation function in two cases: heat conduction and fluid flow problems. Cubic B-spline test function is employed because it is superior to approximation of linear and non-linear problems. We investigated the accuracy of the numerical formulation and focused on the position of the breakpoints within the computational domain. When the domain is divided by partitions of equal space, the results show poor accuracy. For the case of a heat conduction problem this partition can not reflect the temperature gradient which is rapidly changed near the wall. To correct the problem, we have more grid points near the wall or the region which has a rapid change of variables. When we applied the unequally spaced breakpoints, the results show high accuracy. Based on the comparison of the linear problem, we extended to the highly non-linear fluid flow problems.

• 한국가시화정보학회지
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• 제4권2호
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• pp.3-5
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• 2006

Recently, the next-generation advanced flow visualization techniques such as holographic PIV, aynni.c PIV, echo-PIV, micro/nano-PIV, and X-ray PIV have been introduced. These advanced mea-surement techniques have a big potential as the core technology for analyzing outmost thermo-fluid flows in future. They would be indispensable in solving complicated thermo-fluid flow problems not only in industrial fields such as automotive, space, electronics, aero- and hydro-dynamics. steel, and information engineering, but also in the research fields of medical science, bio-medical engineering, environmental and energy technology etc. Especially, NT (Nano Technology) and BT (Bio Technology) strongly demand these advanced measurement techniques, because it is impossible for conventional measurement methods to observe the nano- and bio-fluidic flow phenomena. In this article, the basic principle of these high-tech flow visualization techniques and their practical applications which cannot be resolved by conventional methods, such as blood flows in a micro-tube, in vivo analysis of micro-circulation, and flow around a living body are introduced as a blue ocean strategy.

• International Journal of Aeronautical and Space Sciences
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• 제17권3호
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• pp.423-431
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• 2016

In this study, wing design optimization for long-endurance unmanned aerial vehicles (UAVs) is investigated. The fluid-structure integration (FSI) analysis is carried out to simulate the aeroelastic characteristics of a high-aspect ratio wing for a long-endurance UAV. High-fidelity computational codes, FLUENT and DIAMOND/IPSAP, are employed for the loose coupling FSI optimization. In addition, this optimization procedure is improved by adopting the design of experiment (DOE) and Kriging model. A design optimization tool, PIAnO, integrates with an in-house codes, CAE simulation and an optimization process for generating the wing geometry/computational mesh, transferring information, and finding the optimum solution. The goal of this optimization is to find the best high-aspect ratio wing shape that generates minimum drag at a cruise condition of $C_L=1.0$. The result shows that the optimal wing shape produced 5.95 % less drag compared to the initial wing shape.

• 조명전기설비학회논문지
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• 제14권6호
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• pp.58-68
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• 2000

본 논문에서는 다대식 가열로내의 산소 농도 변화를 표현하는 모델이 제안되었다. 설계된 모델은 크게 '잔류 가스에 대한 모델'과 '산소에 대한 모델'의 두가지로 구성되었다. 각각의 모델은 산소농의 변동에 관여하는 네가지 요인들올 화학, 유체 이론적 관계식과 퍼지 이론을 이용하여 설계되었다. 고려된 네가지 요인들은 버너에서 의 연소반응, 연소대간의 유체 이동, 가열로 내부로부터 외부로의 유체 흐름 및 출입구를 통한 외부 공기의 유입 등이다. 모의 실헝 결과블 통해 제안된 모델로 계산된 각 연소대내의 산소 농도 변화가 설제 조업시 발생하는 유형과 유시함을 알 수 있었다.